Combustion aid for a compression ignition engine

ABSTRACT

This disclosure deals with an internal combustion engine of the compression ignition type, including an improved combustion aid for facilitating starting of the engine and for reducing white smoke (unburned fuel in the exhaust) during starting and operation. The improved combustion aid includes a fuel burner located in the engine air intake, the products of combustion from the fuel burner flowing to the inlet ports of the cylinders. These products of combustion mix with and heat the primary combustion air passing through the air intake. Such preheating combined with the temperature increase resulting from compression in the engine cylinders insures rapid ignition and complete combustion of the injected fuel to effect prompt starting of the engine and early elimination of white smoke. For starting and operation, the burner may be started and stopped automatically under the control of a thermostat responsive to the temperature of the engine coolant at a point where the coolant either enters or leaves the engine block. A system is also provided for supplying the burner with fuel and air and for regulating the flow of fuel and air in response to certain engine parameters. This disclosure also relates to an improved fuel burner that may be used to start either low compression ratio engines or conventional high compression ratio engines.

ilnited tates Kaine [151 3,687,122 [451 Aug.29,1972

[ COUSTEON FOR A COSHON IGNITION ENGINE [72] Inventor: Roy Kama, Columbus, Ind.

[73] Assignee: Cu Engine Company, Inc.,

Columbus, Ind.

22 Filed: July 28, 1970 21 Appl.No.: 58,920

Related US. Application Data [63] Continuation of Ser. No. 801,710, Feb. 24,

1969, Pat. No. 3,526,214, which is a continuation-in-part of Ser. No. 685,103, Nov. 22, 1967, and a continuation-in-part of Ser. No. 685,106, Nov. 22, 1967.

[52] US. Cl ..123/122 G, 123/142.5, 123/179 H, 60/13, 431/19 [51] lint. Cl ..F02m 31/04 [58] Field of h ..123/l22 G, 142.5, 179 H; 60/13; 431/19, 265, 350, 351

[56] References Cited UNITED STATES PATENTS 1,902,930 3/1933 Zubaty 123/139 AV 2,171,209 8/1939 Folsom 123/139 AV 2,633,698 4/1953 Nettel ..60/1 3 1,387,848 8/1921 Good ..l23/l22 G 3,397,684 8/1968 Scherenberg 123/ 142.5 1,625,629 4/1927 Scott ..431/265 X 1,994,968 3/1935 Sloyan ..431/265 2,654,991 10/1953 Nettel ..60/13 2,796,118 6/1957 Parker et al ..43l/265 X 2,993,487 7/1961 Konrad et a1 ..123/l42.5

AIR PRESS.

363 FUEL PUMP coMP.

3,158,192 11/1964 Mizer ..123/142.5

Primary Examiner-Laurence M. Goodridge Attorney-Hibben, Noyes & Bicknell [57] ABSCT This disclosure deals with an internal combustion engine of the compression ignition type, including an improved combustion aid for facilitating starting of the engine and for reducing white smoke (unburned fuel in the exhaust) during starting and operation.

The improved combustion aid includes a fuel burner located in the engine air intake, the products of combustion from the fuel burner flowing to the inlet ports of the cylinders. These products of combustion mix with and heat the primary combustion air passing through the air intake. Such preheating combined with the temperature increase resulting from compression in the engine cylinders insures rapid ignition and complete combustion of the injected fuel to effect prompt starting of the engine and early elimination of white smoke.

. gine parameters.

This disclosure also relates to an improved fuel burner that may be used to start either low compression ratio engines or conventional high compression ratio engines.

15 Claims, 22 Drawing Figures FUEL FROM VlBRATOR HIM/HI"- THERMA 3 5 SWITCH PATENTED M1829 I972 3.687.122

sum 010F 11 PATENTED M1829 I972 SHEET 02 HF 11 I IIIA '4 PATENTEflAuszs m2 3.6 87.122

sum oaur 11 PATENTEDMIE I912 3.687.122

SHEET OSUF 11 PATENTED AUG 29 m2 SHEEI OBUF 11 COIWBUSTION AID FOR A CORESSION IGNITION ENGINE CROSS-REFERENCE TO RELATED APPLICATIONS This application is a continuation of application Ser. No. 801,710 filed Feb. 24, 1969, now US. Pat. No. 3,526,214, which is a continuation-inpart of application Ser. Nos. 685,103 and 685,106, filed Nov. 22, 1967.

BACKGROUND OF THE INVENTION In an internal combustion engine of the compression ignition or diesel type, the air entering the cylinders in each cycle must be compressed sufficiently to raise the air temperature above the temperature necessary to effect reliable and complete combustion under all normal conditions of service use. This has placed limitations on the minimum compression ratio (cylinder volumes in the down and up positions of the piston) that may be used while insuring reliable starting, smooth idling and the early elimination of white smoke, that is, the unburned fuel vapor which remains suspended in the exhaust gas until a sufficiently high temperature has been attained. Thus, compression ratios of 16 to l and above are most commonly employed in conventional engines of the size range intended for on highway vehicle operation at very low ambient temperatures. Such engines have sometimes been equipped with various kinds of heaters burning engine fuel within the air intake to raise the temperature of the intake air through the relatively small range required to insure reliable starting at sub-zero temperatures, the burner being stopped after the starting.

Much effort has been directed particularly in recent years to the development of a diesel engine of the size intended for on highway use and having a low compression ratio of, for example, 12 to 1. With such an engine it is possible to increase the power output or reduce the engine stresses of a diesel for a given size and weight. In a low compression ratio engine, a greater mass of air may be forced into the cylinders by supercharging or turbocharging, and a correspondingly greater amount of fuel may be burned in each cycle without exceeding the permissible peak combustion pressure. Conversely, when less than the maximum permissible air and fuel are injected into the cylinders, lower engine stresses will be encountered and the engine will have a longer life and greater reliability.

A major problem impeding the development of a low compression ratio engine has been the excessive production of white smoke, particularly at starting, idling, and low load operation.

White smoke comprises unburned fuel droplets which escape in the exhaust from the cylinder. It occurs when the temperatures in some portions of the cylinders are insufficient to burn the fuel therein, as for example when an engine is being started and the temperature distribution of the intake air supplied to the cylinders is uneven. White smoke thus differs materially from black smoke, which comprises carbon particles resulting when the compression temperature is adequate to support combustion, but the local oxygen supply is insufiicient to oxidize all the carbon in the fuel.

Another problem with low compression ratio engines is that they are more difficult to start than high compression ratio engines. This is due to the difficulty in obtaining a high enough compression temperature to effect ignition of the fuel-air mixture anywhere in the cylinders.

British Patent No. 772,298 and Lieberherr US. Pat. No. 3,257,797, suggest that fuel burning preheaters may be used to supply additional heat for starting of engines with such low compression ratios. However, these preheaters have not successfully coupled starting capability with the early elimination of white smoke.

In an effort to increase specific output, the industry has at great expense directed its efforts toward the perfection of engines having a variable compression ratio piston. This comprises a number of parts shiftable relative to each other in response to pressure changes within the cylinder so as to provide the high compression ratio required for starting idle and low load operation, and a lower compression ratio during operation of the engine under load. In spite of its apparent acceptance by experts in the field, the variable compression ratio piston has numerous disadvantages and has not yet achieved real commercial success.

' RY OF THE INVENTION The present invention provides a combustion aid for facilitating starting of a diesel engine and for eliminating white smoke. These benefits are achieved by providing a burner in the air intake of the engine, the hot gases, such as the products of combustion, from the burner flowing to the air intake ports leading to the engine cylinders. In addition, the invention resides in a novel means of automatically starting and stopping the fuel burner, and for regulating the flow of fuel and air to the burner.

By efficient utilization of the heat developed by the burner, the amount of fuel required to be burned, even in an engine of low compression ratio, is so small that the air drawn into the manifold and each of the cylinders will not be robbed of such quantity of its oxygen as would interfere either with efficient and immediate ignition of the fuel as injected into the cylinders or the rapid elimination of white smoke during the starting.

The invention also contemplates an internal compression engine of the compression ignition type, including a burner for heating the engine intake air and having a generally cup-shaped enclosure; a compression ignition engine having a relatively low compression ratio, and a burner for heating the engine intake air and burning fuel at a rate which is related to the size of the engine; and a compression ignition engine including a burner having a nozzle connected to receive fuel from a constant level fuel supply and connected to a compressed air supply for aspirating fuel from the fuel supply into the nozzle.

The invention also resides in the novel construction of a fuel burner to start low compression ratio and high compression ratio engines.

BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a side elevational view showing an engine embodying the invention;

FIG. 2 is a fragmentary sectional view taken along the line 2-2 of FIG. ll;

MG. 3 is a fragmentary perspective view of a part of a combustion aid of the engine shown in FIG. 1',

HG. 4 is a fragmentary cross-sectional view of the engine taken on the line 4-4 of FIG. 2;

FIG. 5 is a fragmentary sectional view taken along the line 5-5 of FIG. 4;

FIG. 6 is a fragmentary cross-sectional view taken along the line 6-6 of FIG. 2;

FIG. 7 is a fragmentary cross-sectional view taken along the line 7-7 of FIG. 6;

FIG. is an enlarged cross-sectional view taken along the line 8-8 of FIG. 2;

RIG. 9 is a fragmentary cross-sectional view taken along the line 9-9 of FIG. 12;

FlG. ill is a fragmentary cross-sectional view taken along the line ill-l0 of FIG. 41;

FlG. llll is a cross-sectional view taken along the line lllll ofFIG. 1%;

FIG. 12 is a perspective view of the water circulating system of the engine shown in FIG. 1;

H6. 13 is a schematic view of the fuel and air supply system for a fuel burner for the engine shown in FIG. 1;

FIG. i4 is a fragmentary top elevational view showing a preferred form of a combustion aid embodying the invention;

MG. 15 is a fragmentary side elevational view of the combustion aid shown in F IG. 14;

FIG. :16 shows an alternate form of a combustion aid;

FIG. 117 shows schematically a wiring diagram for the fuel burner of the engine shown in FIG. 1;

FIG. l8 is an alternate form of a fuel supply apparatus and control for a fuel burner;

FIG. l9 shows a fuel burner embodying the invention; and

FIGS. 26) to 22 show curves illustrating the operation of an engine embodying the invention.

While the present invention is applicable to both two-cycle engines and four-cycle engines, a four-cycle diesel engine of the V-type is illustrated and described herein. As shown in FIGS. 3 through 13, the cylinders 2 51 are arranged in two banks in a block 240 and covered by heads 242 with pistons 243 reciprocable in liners 244 therein by connecting rods 245 journaled on a central and properly counterweighted crankshaft 246. Numerous intercommunicating water passages 247 and 248 (FIGS. 4 and 9) are formed in the block and heads around the cylinders 250 and extend between an inlet conduit 249 (FIG. 12) leading to a manifold 25 l on the block and conduits 252 at the outlets of the head passages 248 (FIGS. 2 and 12).

Camshafts 253 (FIG. 4) journaled in the engine block and driven in timed relation with the crankshaft are connected by conventional linkages 254 (FIG. 8) to operate fuel injectors 255, air intake valves 256 and exhaust valves 257 at appropriate times in each engine cycle in accordance with naturally aspirated or turbocharged engines, as the case may be. While the intake valve 256 of a cylinder is open, air is drawn in through a passage 258 into the cylinders as shown in FIGS. 2 and When an exhaust valve is open, exhaust gases are discharged through a port leading to the exhaust manifold 27%. In the particular form of the engine illustrated, in each bank of six cylinders 250, indicated in dashed lines in FIG. 2, four intake passages 258 are provided. The passage 258 at each end of the block conducts intake air to only one cylinder, such cylinders being the associated endrnost cylinders. Each of the other two innermost passages 258 conducts intake air to two cylinders. As shown in FIG. 2, each of the two innermost passages is in the shape of a Y and intake valves 256 for two adjacent cylinders are located at the ends of the branches of the Y.

The crown of each piston is formed with a central recess indicated by the line 259 in FIG. 8, and the fuel injected into the cylinder is sprayed into this recess. The fuel charge for each cylinder is thus mixed with the air then filling the cylinder, the air having been heated, under normal. load conditions, as a result of compression on the upstroke of the piston to a temperature suf ficiently high for ignition of the fuel.

The fuel charge injected into the successive cylinders of each bank is derived from a supply tank 261 (FIG. 13) pressurized by an engine driven pump 262 and delivered through a valve 263 opened by energization of a solenoid 264 to the injector supply rails 265. The excess fuel is returned to the pump inlet through a rail 266.

Where, as in the illustrated embodiment, optimum power output for an engine of given size is a prime objective, provision is made for compressing the intake air when the engine is operating under load and cooling the compressed air before it enters the cylinders. Such supercharging is effected by a so-called turbocharger 267, preferably one for each bank of cylinders, comprising a compressor 268 driven by a turbine 269 (FIG. 1) and operating to draw air through openings 271 (FIG. l) and, after compressing and thereby heating the air, discharging the same through a conduit 272 into the top and at the center of the manifold 273 of the cylinder bank. The turbocharger units may be mounted on top of the engine above the heads of the respective banks of cylinders. The turbine 269 of each turbocharger 267 is driven by exhaust gas passing from and flowing out of the exhaust manifold 274 (FIG. 4) of one bank of 1 cylinders to a conduit 275 and then to and through the turbine. For high power output, it is preferred that each turbocharger have sufficient capacity to boost the pressure by a factor of at least 3 to 31, that is, to nearly 45 psia and, with such a pressure boost, a cooler is preferably provided to attain maximum power output to improve engine efficiency. A turbocharger providing a pressure boost of 2 to I may be used with a correspondingly lower power output and, in such instance, a cooler may not be necessary.

In the present instance, the illustrated engine is designed for optimum power output for which purpose the intake air leaving each compressor 267 through the associated conduit 272 is cooled substantially when the engine is operating under load. This is accomplished by a heat exchanger 276, one for each bank of cylinders, extending along the full length of the associated air intake manifold 273 and disposed in the upper parts of the chambers 277 defined thereby. The exchangers (FIGS. 6 and 12) comprise headers 278 and 279 at opposite ends of and communicating with parallel pipes 281 from which radiate closely spaced rectangular fins 282 slightly smaller than the inlet cross-section of the manifold chamber 277. The exchanger unit is mounted through the medium of a flange 283 (FIG. 4).

Water may be used as the engine cooling medium and circulated through a system (FIGS. 1, 9 and 12) which includes a pump 284 driven from the engine crankshaft and a radiator 285 cooled by a suitable engine drive fan 286 and having inlet conduits 287 communicating with the casings 288 of thermostatic valves 289 (FIGS. 9 and 12). The outlets 252 from the water passages 248 of the heads are connected to the bottoms of the casings 288 as shown in H6. 9. Some or all of the pumped water may by-pass the radiator through a conduit 295 having branches 296 leading from the casings 288. The radiator outlet extends through a conduit 291 to the inlet of the pump which forces water through a conduit 292, an oil cooler 293 and the conduit 249 into the water manifold 251 of the engine. From the inlet end of this manifold water may flow through the conduits 249a to the respective headers 278 through tubes 281 of the respective heat exchangers 276 and through pipes 294.

Alternatively and preferably for some engines, the tubes 281 of each heat exchanger 276 and the water manifold 251 may be connected in series between the pipe 249 and the casings 288. Thus, instead of the water flow from the pump being divided and passed part through the tubes 28l and the remainder through the engine jackets, all of the water may flow first through the heat exchanger tubes and then through the engine jackets.

Distribution of the water flow through the radiator and the by-pass conduit 295 is determined by the valves 289 (FIG. 9) herein disposed within the casings 288 and movable back and forth with changes in the temperature of the water at the junctions of the heads and exchanger outlets 252 and 294 and the by-pass 295. i-lerein, each valve comprises a sleeve 297 coupled at 293 to the movable end 302 of a thermostatic bellows 299 disposed within a chamber 301 and anchored at 34B. The chamber communicates with the head and exchanger outlets so that the actuator moves the sleeve between the positions shown in full and in phantom in F IG. 9 when the sensed temperature is above and below a range predetermined by the construction and setting of the actuator 299. With this arrangement and when the temperature of the flowing water is above the upper limit of the range, for example 195 F., the sleeve end 297 will be positioned against a seat 297a as shown in full in FIG. 9 thus closing the inlet to the by-pass conduit 295 and fully opening the passage between the inlets 252 and 294 and the radiator inlet 287. All of the water circulated by the pump thus flows from the engine jackets and the heat exchangers and through the radiator so as to be subjected to maximum cooling.

When the engine is cold, the thermostatic actuator 299 senses a temperature below the selected range, for example 180 1 and moves the sleeve downwardly to the position shown in phantom in FlG. 9, the radiator inlet passages 287 are closed and all of the circulated water flows through the by-pass to the pump and then through the exchanger coils and engine jackets back to the thermostat casing 288. The radiator is then inactive and does not withdraw any heat from the circulating water. At temperatures of the water intermediate the limit values mentioned above, the valve sleeve will be disposed in corresponding positions between those shown in full and in phantom and the circulated water flow will be divided between the radiator and the bypass 295.

From the foregoing, it will be apparent that the thermostatic valves 289 operate continuously and automatically to maintain maximum water flow through the radiator and therefore maximum cooling when needed during operation of the engine under full load. But, when the engine is cold or the heat of combustion Within the cylinders during starting or idling can best be utilized for maintaining smooth engine operation at the low compression ratio, the radiator is completely disabled or partially disabled by partial opening of the valve 289 by the thermostatic actuator 299. Thus, for a substantial period after starting, the heat absorbed from the engine by the circulating water is utilized through the medium of the heat exchangers 276 to assist in heating the manifold air in the continued operation of the engine.

The engine is designed for operation at a fixed compression ratio of 12 to l, substantially lower than the ratio now used in most commercial engines. That is to say, the ratio of total cylinder volume Vt (H6. 8), with the piston down, to the clearance volume Vc with the piston up, is relatively low.

It is difficult to rapidly start and reduce white smoke from a low compression ratio engine except at very high ambient temperatures. The temperature resulting from compression within the cylinders at lower ambient temperatures are not high enough to effect complete burning. This, of course, is because the heat added to the air by compression within the cylinders, minus the heat lost to the surrounding cold metal, results in an air temperature which is below the temperature required for complete combustion.

The utilization of a low compression ratio in a mu]- ticylinder diesel engine to provide substantial power output or prolonged service life is made possible in accordance with the present invention by burning engine fuel at an accurately metered rate within the manifold chamber 277 and directing the flow of the developed heat to and distributing the same between the engine cylinders in a novel manner such as to heat, quickly and consistently under all starting conditions, all of the admitted air to a temperature sufficiently high to produce, within each cylinder, a compression temperature which is sufficiently above the theoretical temperature required by the fuel to insure rapid ignition and which is sufficiently uniform throughout the air charge to insure rapid elimination of white smoke, or unburned fuel in the exhaust. The fuel burning in the manifold chamber is started instantaneously with cranking and at a rate sufficient to attain within the cylinders quickly and without fail under all expected conditions of cold starting and operation a compression temperature well above that necessary for rapid ignition and the early elimination of white smoke.

Burners 33M, supplied with the engine fuel at a proper flow rate and constructed and mounted in the manner shown in H68. 2, 3, 5 to 7 and H3 enable the engine as above described, to be started in a few seconds, for example it) seconds, of cranking and at the same time insuring the disappearance of white smoke in the exhaust within no more than 40 seconds even at an ambient temperature as low as -25 F.

The burner 304 for one bank of cylinders comprises two nozzles 305 from which a mixture of compressed air and atomized fuel is discharged into the ends 3&6 of tubes 3%? disposed within the manifold chamber 277 below the heat exchanger 276 and disposed adjacent and extending along the inner wall 308 of the manifold chamber close to ports 309 therein leading to the intake passages 258. The tubes are a compound of metal and are formed with side openings 31 l opposite each of the ports 309 and passages 25%. The ends 306 of the tubes 307 are joined by bars 312 (See FIG. 3). The other ends of the tubes project through the end walls 313 of the manifold and are located by fittings 3 id.

The nozzles are threaded into opposite sides of a casting 3H5 at the inner end thereof, the casting projecting through a hole 316 in the outer wall of the manifold and in between the bars 312. The casting is formed intermediate its ends with a flange 317 screw clamped against this wall. Herein, the tubes at one end of the block communicate with each other through a pipe 318 (FIG. 13) to always equalize the pressures between the two manifolds.

liach nozzle 305 comprises a cup 319 threaded at 321 into the side of the casting 315 and having a hole 322 aligned with an orifice 323 at the end of a sleeve 324 disposed within and threaded at 325 into the cup. A plug 326 pressed into the outer end of the sleeve is formed with a passage 327 terminating in the orifice 323 which is spaced a short distance from the inner end of the hole 322. A frusto-conical surface 328 on the end of the plug cooperates with the inner surface of the cup to form an annular air passage 329 which converges toward the hole. The plug 326 may be replaced by one having an orifice 323 of a different size corresponding to the burner output that may be required for another engine.

Fuel for each of the two burners is supplied to the inner ends of the sleeves 324 through a passage 331 in the casting 315 and a chamber 332 between seal rings 333 around the sleeves 324. The outer end of the passage is disposed below the level of fuel maintained in a closed tank 334 (FIG. 6) clamped against the outer wall of the manifold. The pressure in the tank is equal at all times to the prevailing manifold air pressure by virtue of a passage 336 (FIG. 6) establishing continuous communication between the two.

The level of the fuel within the tank is maintained constant by any well-known mean. Herein, fuel under some pressure in the return line 266 (FIG. 13) is supplied to the tank through a pipe 335 and a valve 336 having a member 339 bearing against an arm 337 on a float 34h pivoted at 338 and resting on the fuel within the tank. Fuel is admitted to the tank when the valve is open but the flow is interrupted when, by a rise in level, the member 339 becomes seated as shown in FiG. 6.

Air for aspirating fuel outwardly through the orifice 323 and atomizing such fuel is delivered through respective burners to passages 3M terminating in chambers 342 within the casting 3l5 and around the sleeves 32 i and communicating through grooves 353 along the sleeves and plugs 326 with the converging passages 329. Air is supplied from any suitable source at a pressure which is sufficiently higher than the manifold pressure to produce an adequate flow for aspirating fuel at the proper rate through the orifice 323, for properly atomizing such fuel and for supplying a proper proportion of the air needed for combustion of such fuel,

Because of the high speed atomizing air, the nozzle 303 provides excellent atomization of the fuel, is not prone to clogging, and operates at relatively cool temperatures.

Air for the manifold burner may be derived from various sources such, for example, as a compressor driven by a separate motor when the burners are to be operated and adjusted to deliver air at the desired pressure. Or, in the case of transport vehicles, the air may be supplied from the tank 34 (FlG. 13) that supplies the vehicle air brakes. In such a case, a suitable automatic reducing valve ass (FIG. E3) of well-known construction is used and adjusted to provide the desired constant pressure within the passage 332 when a valve 347 is opened by energization of a solenoid Iidfl.

With the construction above described and while compressed air is being supplied, fuel will be aspirated through the orifice 323 at a rate determined by the orilice size, the air pressure, the difference in the level between the tank 33d and the nozzle 3&5 and the pressure within the manifold chamber 277. The latter may be disregarded since, at times when the burners are to be active, such as during starting or idling, the turbocharger is not producing any appreciable increase in the manifold pressure. The constant pressure air flow is thus utilized not only to atomize the burner fuel but also to aspirate the fuel from the constant level tank and to meter the fuel supply accurately in proportion to the rate of air flow Thus, the heat of the burner herein shown is always constant.

Ignition of the atomized fuel-air mixture discharged from each burner nozzle in a flaring pattern is efi'ected by sparks spanning the gap 349 of a spark plug 350 mounted on the flange 327 with the gap positioned near the burner noule and in the path of the atomized mixture. The sparking is produced in the usual way as by a conventional ignition coil and a vibrator.

The formation of the heater flame within a tube of the above construction and of smaller cross-section than the manifold while extending the tube along the intake ports 258 in close proximity thereto is advantageous for several reasons. The flame is confined to a zone close to the intake ports so that the flaming mixture is delivered quickly and uniformly into the ports as each intake valve is opened. During starting, the flame does not come into contact with the walls of the manifold chamber 277 thus minimizing heat losses to these parts. Also, the imperforate top of the tube insulates the burner flame and shields the heat exchanger 276 from the heat developed in the tube and reduces the radiation thereto so as to reduce the spacing needed to avoid any danger of damaging the exchanger. The imperforate top of the tube also reduces the danger that the flame will be blown out by the stream of intake air flowing through the manifold.

FIGS. lid and 15 show a preferred form of combustion aid and one adapted for use in a V-8 engine in which the air intake ports and the intake manifolds are located within the V of the engine block and supplied with air through inlets disposed intermediate the ends of the manifolds and the banks of cylinders. in such an engine, the center lines of the cylinders of each bank may be at a 45 angle from a vertical line. FIG. 14 is a horizontal sectional view through the manifold of such an engine, looking downwardly from a plane immediately above the burner, and FIG. 15 is a vertical sectional view looking toward the burner from a vertical plane adjacent the burner. Mounted within the manifold 416 is a burner comprising a nozzle 423 of the character previously described mounted on a holder block 424 secured to one end wall of the manifold and having the air and fuel passages formed therein. The holder 424 also supports a spark plug 426 having its points 427 located adjacent the nozzle 423 in order to ignite a fuel-air mixture issuing from the nozzle 423.

The aid further includes a heat distributor comprising an open ended metal tube 428 which is secured to the wall of the manifold 416 by a pair of straps 429 and 4341 and is positioned in axial alignment with and adjacent the nozzle 423, so that an air-gas mixture issuing from the nozzle enters the adjacent end of the burner tube 428. The latter extends along and is disposed adjacent the intake ports 417 to 420 and has side openings 432 to 435 which are respectively located adjacent and opposite the intake ports 417 to 420.

In order to improve quick starting of the engine and early elimination of white smoke it is desirable to uniformly distribute the heat from the burner to the respective intake ports. For this purpose, the tube 428 is mounted closely adjacent to and extends across the ports 417 to 420, and the openings 423 through 435 of the tube 428 are sized and located relative to the intake ports 417 to 420 so that all of the intake ports receive substantially equal amounts of the heat delivered by the burner. This is accomplished mainly by progressively increasing the areas of the openings 432 through 435 with increasing distance from the nozzle 423. Thus, the opening 432 which is closest to the nozzle 423 is relatively small and the leading edge 437 of the opening 432 is approximately in line with the leading side of the port 417. The next opening 433 is slightly larger than the opening 432 and its leading edge 438 is a short distance nearer the nozzle 423 than the leading edge of the port 418. The next opening 434 is larger than the other two openings 432 and 433, and its leading edge 435 is a greater distance nearer the nozzle 423 than the adjacent edge of the port 419. Finally, the opening 435 is larger than any of the other three openings 432, 433 and 434, and its leading edge 440 is advanced even nearer the nozzle 423 than the leading edge of the port 421). Thus, the gradually increasing sizes of the openings with increasing distances from the nozzle results in a uniform distribution of burner heat to the various cylinders. The flaming mixture from the nozzle 423 sweeps upwardly as seen in FIG. 15 and toward the right, and the advance of the leading edges 437 to 440 relative to the ports 417 to 420 permits the hot gases in the form of flame and heated air to sweep into the ports 417 to 42!).

In addition to the air supplied to the nozzle 423 to aspirate the desired constant flow therethrough and effect proper atomization, it is important that the burner receive additional air in order to effect complete combustion of the burner fuel. This may be accomplished, for example, by a plate 442 supported on the burner holder 424 by boits 443, extends across the manifold a short distance beyond the end of the nozzle 423 and close to the inlet end of the burner tube 428. The plate 442 has a central hole 444 axially aligned with the nozzle 423. A spray of fuel and air discharges from the nozzle, through the opening 444 and into the end of the burner tube. The edge of the hole 444 may be tapered inwardly and toward the tube 428 to form a venturi. By ejector action, enough air is induced to flow from the surrounding manifold space into the burner tube to provide for substantially complete combustion of all of the atomized fuel. The resulting flame and products of combustion flow through the tube 428 and laterally out of the tube through the holes 432-435 and into the intake ports 417 to 420.

A relatively small part of the air flowing into the manifold through the hole 444 enters the burner tube. The remainder of the intake air flows transversely across and around the burner tube 428, becomes heated by contact with the burner tube 428 as it approaches the intake ports, and becomes mixed with the products of combustion leaving the openings 432 to 435 as illustrated in FIG. 15. As shown in FIG. 15, the burner tube 428 is positioned somewhat below the level of the ports 417 to 420 so that the tube does not block the downward flow of intake air into the intake ports 417 through 421).

FIG. 16 illustrates a combustion aid embodying the invention, including a single tube 451 which extends adjacent all of the cylinder intake ports 452 and 453 along one side of the engine. The tube 451 is supported from opposite ends on fittings 454 (only one shown) which project from opposite end walls 456 of the manifold 457. A nozzle 458 of the same construction as the nozzles previously described is threaded into the fitting 454 and supplied with fuel through a pipe 459 and with atomizing air through a surrounding passage 461 so as to project a spray of fuel into the tube 451. A spark plug 462 is provided to ignite the fuel. The tube 451 has a plurality of relatively small holes 463 formed therein throughout its length. The perforated area of the tube 451 consists of approximately two-thirds of its circumference, approximately one-third of the tube circumference on the up-stream side thereof being imperforate in order to prevent the flame from being blown out by the flow of intake air and to protect an intercooler (not shown) from the burner heat. The portion of the holes 463 adjacent the nozzle 458 and adjacent the upstream side of the tube 451 permit a portion of the intake air to flow into the tube 451 and mix with the sprayed fuel, and the portion of the holes 463 on the downstream side of the tube permit the flame and products of combustion to flow out of the tube and into the intake ports.

Additional or larger holes could be provided adjacent the nozzle 458 if additional intake air is needed for complete combustion. To obtain an even distribution of heat to the various cylinders, the total area of the holes 463 per unit length of the tube is gradually increased with increasing distance from the nozzle 458. While this could be accomplished by having a uniform number of holes and gradually increasing the size of the holes, in the present instance it is accomplished by keeping the hole size uniform and increasing the number of holes with distance from the nozzle 458. Thus, the combustion aid shown in FIG. 16 evenly distributes the bumer heat similar to the operation of the aid shown in FIGS. 14 and 15.

in another of its aspects, the present invention contemplates stopping the manifold burner automatically at the proper time after each starting of the engine and again turning the burner on whenever, as during a period of idling or low load operation, the heat of combustion is insufficient to maintain a compression temperature sufficiently high to prevent rough operation of the engine or the reappearance of white smoke in the exhaust. Since it is not practical to measure the actual compression temperature within the engine cylinders, an equivalent or indirect and corresponding temperature measurement is made at a point in the overall system where all of the several factors affecting the actual compression temperature are combined so that a single temperature reflects and corresponds quite closely to the changing value of the compression temperature. Among such factors that prevail during idling are the heat of combustion, the residual heat held in the engine parts and in the cooling system, compression ratio and the prevailing ambient temperature.

I have discovered that the temperature of the water continuously circulating either in the radiator or bypass paths above described or in both of such paths is influenced by all of the above factors, particularly at a point in the flow path of the water through the circuit including the by-pass 255 when the radiator is inactivated by the action of the thermostat. The sensing element 353 of a thermostat 354 for measuring such temperature changes may, as shown in FIGS. 1t) and 12, be disposed at the inlet to the water manifold 251 which communicates with the engine and intercooled passages.

The thermostat 354 may be of the construction (PIG. ll) sold by Fenwall Incorporated under the trade designation MC 177D and including the sensing element 353! in the form of a shell which expands and contracts with changes in the water temperature. Non-expanding struts 355 disposed within and anchored to opposite ends of the shell carry contacts, forming a switch ass which operates with a snap action and is closed as shown in FIG. 1 1 when the water temperature falls below a predetermined value, for example 180 F., and is opened when a somewhat higher temperature, for example 195 F., is sensed. By adjusting a screw 357, the temperature range of the thermostat may be varied in accordance with the requirements for a given engine.

The starting and stopping of the burner 304; in conjunction with the starting, stopping, idling and full load operations of the engine above described may be controlled by the circuitry shown in FlG. l7. When the engine, and therefore the coolant, is cold, the thermostat switch 356 will be closed and the valve sleeve 297 will be disposed as shown in phantom in FIG. 9 thus disconnecting the radiator and fully opening the by-pass 295. To start the engine, a key 357a is turned to first close a switch 352% and energize the solenoid 264 for opening the valve 263 interposed in the line 265 leading from the fuel pump 262 to the injectors 255. Further turning of the key closes a switch 359 which energizes a solenoid 36E to start the cranking motor 362. Closure of the switch 358 enables current flow through the then closed switch 356 and starts the distributor motor 352, activates the ignition coil unit 351, and energizes a solenoid 343 for opening the valve 347 to admit air from the pressure source 344 to the burner nozzles 3%. Thus, immediately with the start of the cranking,

l2 the combustible sprays of fuel and air are discharged from the nozzles 305 and ignited to form flames directed into the ends of the tubes 3G7 and along the latter as illustrated in FIG. 5 to provide the proper amount of heat for immediate ignition in the manner detailed below.

As soon as the engine starts, the key 357a is released to allow the switch 350 to open and stop the cranking motor 362. The switch 353 remains closed so as to continue the energization of the fuel pump solenoid 264, and also energization of the air valve solenoid 348, the distributor motor 352, and the ignition coil 351 through the then closed thermostat switch 356. Operation of the burner is thus continued.

As the engine is warming up and taking on load, some of the engine heat is transferred through the cylinder walls and absorbed by the water being circulated through the by-pass circuit above described. Thus, after a short warm-up period, the temperature of the water will be raised enough to cause opening of the thermostat switch 356 which results in deenergization of the solenoid 348, the motor 352 and the ignition coil 351 thus interrupting the air flow and shutting the burner off automatically.

As the loading of the engine increases, the engine will become hot and the thermostatic valves 289 will be opened to allow an increasing amount of the pumped water to circulate through the radiator. At full load, the valves will become positioned as shown in full lines in FIG. 9 and all of the circulating water will flow through the radiator.

When the engine is being operated at low levels as during idling, the heat of combustion transferred to the water being circulated through and cooled by the radiator may not be sufficient to maintain the water temperature above the temperature at which the thermostatic switch 356 remains open. The switch thus closes and effects restarting the burners 364 the same as during starting of the engine as above described. Additional heat is thus supplied to the intake air so as to restore the compression temperature necessary for insuring smooth idling and preventing white smoking. Then, when the engine speed and load are again increased, the switch 356 will open and the burners will be shut off in the manner above described.

FIG. 18 illustrates diagrammatically an alternate fuel supply and control system which may be used with a combustion aid embodying the invention. In this form a nozzle 380 of the type shown in FIG. 7 and a spark plug 381 mounted within the interior of an air intake manifold 382. Fuel is supplied to the nozzle 380 by a conduit 383 and a fuel supply tank 384 which in turn receives fuel from a conduit 386. The latter conduit 336 may be connected to receive fuel from the main fuel pump (not shown) of the engine.

The flow of fuel from the fuel pump to the nozzle 380 is controlled from the tank 384 by a valve 337, and a regulator 357. The valve 387 is connected in the conduit 386 between the tank 384 and the main fuel pump, the valve 387 being solenoid actuated and being closed only when the solenoid is energized. Energization and deenergization of the solenoid to open and close the valve 387 is controlled by a float 388 within the tank 384. The float 388 is connected to and supports a post 389 which in turn supports a contact closure plate 391.

A pair of normally open contacts 392 are mounted at the upper end of the tank 384, the contacts 392 being connected in series with the solenoid of the valve 387. The circuit further includes a normally open, manually operable switch 393, a battery 394, and a thermostatically actuated switch 395. As in the case of the switch 356 (FIGS. and 11) above described, the thermostatic actuator for this switch is arranged to respond to a temperature at a point in the overall system which reflects and follows approximately changes in the temperature of the cylinder walls of the engine. As described above, a preferred location of the thermostatic element is near the point where the cooling water leaves the jackets of the engine. The arrangement is such that the switch is normally closed when the engine is cold or the sensed temperature is below a predetermined value below which it is desirable to preheat the air taken into the cylinders.

When the engine start switch 393 is manually closed and the plate 391 establishes an electrical connection between the contacts 392, current flows from the battery 394 through the switches 393 and 395 and the solenoid of the valve 387, thereby energizing the solenoid valve 387 and closing the conduit 386 to fuel flow. The contacts 392 are of course closed only when the plate 391 is moved upwardly by the float 388.

The conduit 383 is connected at 396 to the lower end of the tank 384 below the level of the fuel 390 in the tank 384, and during operation of the burner, air flowing out of the nozzle 389 draws fuel out of the nozzle by an aspirating action. The fuel flow rate to the nozzle 339 is a function of the difference between the nozzle suction pressure and the fuel supply pressure. To keep the fuel flow rate constant, it is also necessary to maintain the above pressure difference at a constant value. Therefore, it is necessary to make the fuel supply pressure a function of the manifold 382 pressure, and this is accomplished by a vent conduit 398, and by the regulator 397 connected in the line 383. The vent conduit 398 runs to both the interior of the tank 384 and to the regulator 397, and the regulator 397 maintains the fuel pressure to the nozzle at a constant relation to the manifold pressure.

Air flow to the nozzle 389 is through another conduit 4l connected to the outlet of a compressor 402. The compressor 492 is driven by a DC motor 493 which is also connected through the switches 393 and 395 to be energized by the battery 394. An air pressure regulator valve 4W3 is connected in the conduit 401 between the nozzle 339 and the compressor 492 in order to regulate the pressure of the air to the nozzle 389. Since the air issuing from the nozzle 339 must be at a certain positive pressure relative to the pressure within the intake manifold 382, the air intake to the compressor 492 is through an intake conduit 496 and from the intake manifold 332. The air pressure regulator valve 494 is also connected to the conduit 496 and thus maintains the pressure in the conduit 491 at a certain value relative to the pressure within the manifold 382.

The circuit for the spark plug 331 comprises the previously mentioned switches 393 and 395 and the battery 394. In addition, the circuit comprises a vibrator 411 and an ignition coil 412. A second coil 413 is also provided, this coil also being connected to the battery 394 and to the vibrator 41 l and adapted to be coni4 nected to the spark plug (now shown) of a burner for another bank of cylinders.

Considering the operation of the system shown in MG. 13, with the engine cold and the switch 393 open, the switch 395 is closed, the fuel pump connected to the conduit 336 is not being driven, the valve 387 is not energized, and the spark plug 381 is not energized. To start the engine, the manually operable switch 393 is closed, such closure causing current flow from the battery 394 through the switches 393 and 395 and through the motor 493. Energization of the motor causes air to be pumped from the air intake manifold 332, through the conduit 4% to the intake of the compressor 402, through the air pressure regulator valve 404, through the conduit 401, and out of the nozzle 380. Such air flow out of the nozzle 380 draws fuel out of the nozzle from the conduit 383 and the tank 384, by an aspirating action. If the fuel level in the tank 384 is initially relatively low, the plate 391 is spaced downwardly from the contacts 392 and the contacts 392 are therefore open. The valve 387 is thus de-energized and permits fuel to flow through the conduit 386 to the tank 384. When the fuel in the tank has risen somewhat, the contacts 392 are closed by the plate 391 and the valve 387 is energized, thus cutting off the flow of ,fuel to the tank 334.

The air issuing from the nozzle 330 atomizes and mixes with the fuel to form a combustible mixture. At the same time, the vibrator 411 and the coil. 412 energize the spark plug 381 and thus ignite the mixture as previously explained. After the engine has started and warmed to a predetermined temperature, the thermal switch 395 opens and de-energizes both the motor 403 and the spark plug 381, thereby turning the burner off. Of course, as previously explained, if the temperature of the engine subsequently falls for any reason, as during idling, the thermal switch 395 again closes and turns the burner back on.

FIG. 19 illustrates a manifold burner 466 in an intake air passage 467 leading to the intake ports of a bank of cylinders (not shown). The burner 466 comprises a cup-shaped enclosure 468 mounted within the passage 467 close to the air intake ports, with its open end facing in the downstream direction. Fuel is supplied to a fuel atomizing nozzle 469 (similar to the nozzles previously described) mounted within the interior of the enclosure 468, by a fuel line 470. The line 470 extends through the wall of the passage 467 and carries fuel from a fuel supply such as a constant level fuel chamber, such as tank 384 (FIG. 18). Also extending through the wall of the passage 467 is an air line 471 which extends from a compressed air supply, such as air compressor 492 (FIG. 18), to the nozzle 469. Conduits 472 and 473 are preferably provided to connect the passage 467 to the fuel and air supplies in order to equalize the pressure therebetween. Inlet openings or vents 474 are formed in the upstream side of the enclosure 463 to permit a portion of the intake air flowing through the passage 467 to enter the enclosure 468 and mix with the fuel and air leaving the nozzle 469. The nozzle 469 is mounted to eject the atomized fuel-air mixture in the downstream direction and this fuel-air mixture is ignited by a spark plug 476. The flame and products of combustion flow out of the enclosure 469 through the large outlet opening 477 of the enclosure 468. The enclosure 468 serves to protect the burner flame against being blown out by the intake air and to create turbulence downstream from the burner in order to thoroughly mix the burner heat with the intake air in order to quickly start an engine.

FIG. 20 illustrates operation of a compression-ignition type engine having a bore between and 6 inches and with an ambient pressure of approximately 14.7 psia, such operation being shown as functions of the compression ratio of the engine and the compression temperature. The line 45 in FIG. 20 represents the compression temperature within the cylinders of the same engine but with various compression ratios when starting the engine with an ambient temperature of 0 F. After cranking, the compression temperature for such engine having a compression ratio of less than 12 to 1 will be less than 580 E., whereas the compression temperature after cranking of such engine having a compression ratio of 18 to 1 will be approximately 725 F. The line 46 in FIG. 20 represents the compression temperature which must be reached within a cylinder in order to sustain firing of a diesel-fuel and air mixture in an engine, and it can be seen that the ignition temperature is higher for engines having a relatively low compression ratio than it is for engines having a high compression ratio. For example, such engine having a compression ratio of less than to l requires a firing temperature of at least 760 F. whereas such engine having a compression ratio of 18 to 1 must have a compression temperature of approximately 725 F. The two lines 45 and 46 intersect at the point 47 which corresponds to a compression ratio of approximately 17.6 to 1, and it will be apparent that a compression ratio of more than 17.6 to 1 is necessary for such engine to start after one minute of cranking time and an ambient temperature of 0 F., without the use of a starting aid.

The line 48 illustrates operation similar to that for the line 45 but with an ambient temperature of 40 F., and it can be seen that such an unaided engine with a compression ratio less than approximately 13.5 to 1 will not start at this ambient temperature.

The line 49 in FIG. 20 illustrates the operation of an unaided engine, when the engine is idling after a period of no load operation with an ambient temperature of 60 F. From this line it will be apparent that for all compression ratios greater than approximately 9.4 to l, the compression temperature will be above that necessary for sustained firing. However, for compression ratios lower than approximately 9.4 to l, the compression temperature falls below that necessary for sustained firing and the engine will stop running.

The line 50 illustrates the operation of such an unaided engine when operating under full load. It will be apparent that the compression temperatures with compression ratios down to approximately 9.2 to 1 will be sufficiently high to sustain firing.

By way of comparison, the line 51 illustrates the operation of a turbocharged engine of the same cylinder diameter, operating under full load, and a comparison of the lines 50 and 51 shows that the turbocharged engine runs considerabiy hotter than a similar engine without turbocharging.

The line 50a represents the upper temperature limit at which white smoke appears. At temperatures above the line 50a, white smoke will be eliminated while at temperatures below the time 50a white smoke will be present.

it can therefore be seen from the curves in FIG. 20

that, if the engine is built having a compression ratio less than approximately l2.0 to 1 and, further, is to start relatively rapidly with ambient temperatures as low as 20 F., is to idle smoothly at such temperatures, and is to operate without white smoke, a combustion aid should be provided. Further to attain high power output from such an engine, a high charge-density boost apparatus should be provided.

As shown in FIG. 21, it is also important that the proper amount of fuel be drawn through the fuel nozzle of the burner for optimum starting results. This mount also rapidly eliminates white smoke. The curve 1 15 is a plot of burner fuel flow rate as a function of the length of time required to start an engine, the curve being based on data obtained from a four-stroke compression-ignition engine having a compression ratio of 12.1 to 1. Further, the engine was an in-line six cylinder engine having a cylinder bore of 5% inches and a piston stroke of 6 inches. The ambient temperature was -15 to 27 F., and the higher heating value of the burner fuel was 19,820 BTU per pound of fuel. As shown by the curve 1 15, the optimum, or minimum, starting time occurs with a burner fuel flow rate of approximately 0.000067 pounds per minute of fuel per cubic inch displacement of the cylinders served by the burner. An air flow rate from the air nozzle of the burner of approximately 10 percent of the amount of intake air flowing through the manifold when starting the engine, provides this fuel flow rate. When more fuel than this amount is fed to the burner, an excessive amount of the oxygen in the intake air will be used up and the air may be excessively vitiated, and when the flow rate is more than approximately 0.000082 pounds per minute per cubic inch displacement, the starting time is very erratic and, in fact, the engine may fail to start. On the other hand, when too little fuel is fed to the burner the intake air may not be sufficiently heated. As shown by curve 1 15, the engine may not start when the fuel flow rate is less than approximately 0.000025 pounds per minute per cubic inch displacement. Thus, the fuel rate should be within the range of from approximately 0.000025 to approximately 0.000082 pounds per minute per cubic inch of engine displacement, for the engine to start. Further, military specifications require that an engine start in less than thirty seconds at -25 E, and therefore a more preferred fuel flow rate is between from approximately 0.000042 to 0.000082 pounds per minute per cubic inch displacement in order to meet military specifications. For optimum performance the rate is approximately 0.000067 pounds per minute per cubic inch displacement.

For a two-cycle engine, it is necessary to increase the fuel flow rate to compensate for the increased air flow. An equivalent optimum fuel flow rate for a two-cycle engine would be about 0.0001 pounds per minute per cubic inch of the cylinders served by the burner.

With reference to FIG. 22, the curve 1 15a illustrates the variation in the amount of oxygen in the intake air consumed by the burner, as a function of the fuel flow rate to the burner. Obviously, as more fuel is fed to the burner more oxygen in the intake air will be consumed. When the flow rate is 0.000082 pounds per minute per 

1. In an internal combustion engine of the compression-ignition type including a plurality of cylinders and air intake means leading to said cylinders, the improvement of a burner located to direct heat in the intake air flowing to said cylinders, said burner including a nozzle, means for supplying air under pressure to said nozzle, means responsive to pressure of air in said intake means for supplying fuel to said nozzle, said nozzle including means for directing air supplied to said nozzle to aspirate fuel from said nozzle and atomize said fuel during operation of said air supplying means, regulator means responsive to variations in pressure in said air intake means for maintaining air pressure at said nozzle at a predetermined pressure above the pressure in said air intake means and for maintaining fuel pressure at said nozzle at a predetermined pressure differential relative to said air intake pressure, and means for igniting said atomized fuel.
 2. The structure as defined in claim 1, wherein said nozzle includes a fuel passage and an air passage which is formed concentrically around said fuel passage.
 3. The structure defined in claim 1, wherein said means for supplying fuel comprises a fuel supply tank, a fuel conduit connecting said tank with said nozzle, and first pressure regulator means connecting said tank and said fuel conduit with said air intake means, and said means for supplying air comprises an air pump, an air conduit connecting the outlet of said pump with said nozzle, and second pressure regulator means connecting said pump and said air conduit with said air intake means.
 4. The structure defined in claim 1, wherein said fuel supply means comprises a tank, conduit connecting said tank to a fuel source, a valve in said conduit for controlling the flow of fuel from said source to said tank, and means in said tank connected to control operation of said valve such that said valve is opened when the fuel level falls to a predetermined level and said valve is closed when the fuel level rises to a predetermined level.
 5. In an internal combustion engine of the compression-ignition type including a plurality of cylinders and air intake means leading to said cylinders, the improvement of a burner located to direct heat in the intake air flowing to said cylinders, said burner including a nozzle, means for supplying air under pressure to said nozzle, means responsive to pressure of air in said intake means for supplying fuel to said nozzle, regulator means responsive to variations in pressure in said air intake means for maintaining air pressure at said nozzle at a predetermined pressure above the pressure in said air intake means and for maintaining fuel pressure at said nozzle at a predetermined pressure differential relative to said air intake pressure, said pressure of said fuel being lower than the pressure of said air supplied to said nozzle, said nozzle including means for directing air supplied to said nozzle to aspirate fuel from said nozzle and atomize said fuel during operation of said air supplying means, and means for igniting said atomized fuel.
 6. In an internal combustion engine of the compression-ignition type including a plurality of cylinders and an air intake leading to said cylinders, the improvement of a burner for heating the intake air flowing through said air intake, fuel supply means connected to supply fuel to said burner, and control means for regulating the flow of fuel from said supply means to said burner, said control means including air intake pressure responsive means for maintaining the pressure of the fuel at a predetermined level relative to air intake pressure, and engine temperature responsive means controlling the fLow of fuel to said burner in response to engine temperature.
 7. The structure defined in claim 6, wherein said engine includes a coolant system, and said temperature responsive means is located to sense the temperature of the coolant in said system.
 8. The structure defined in claim 7, wherein said temperature responsive means is located to sense the temperature of said coolant where said coolant enters the block of the engine.
 9. The structure defined in claim 7, wherein said temperature responsive means is located to sense the temperature of said coolant where said coolant leaves the block of the engine.
 10. The structure defined in claim 6, wherein said engine temperature responsive means for controlling the flow of fuel to said burner includes auxiliary air supply means connected to supply auxiliary air under pressure to said burner, said auxiliary air aspirating said fuel in said burner.
 11. The structure defined in claim 10, where said engine temperature responsive means further includes thermostat means located to sense the temperature of a coolant for said engine, and circuit means responsive to said thermostat means for controlling the flow of said auxiliary air.
 12. The structure defined in claim 10, wherein said control means further includes second air intake pressure responsive means for maintaining the pressure of said auxiliary air at a predetermined level relative to air intake pressure.
 13. In an engine including an air intake for conducting intake air to the cylinders of the engine, the air pressure within said air intake varying during starting of said engine and with various operating conditions of said engine, the improvement comprising a burner located to heat intake air flowing through said air intake, said burner including a fuel nozzle and an air nozzle, means for supplying fuel to said fuel nozzle, means for supplying air under pressure to said air nozzle, said air nozzle being located to aspirate fuel from said fuel nozzle, and pressure regulator means connecting said air supply means with said air intake for maintaining the pressure of air to said air nozzle at a predetermined value above air intake pressure regardless of the operating conditions of said engine.
 14. The structure of claim 13, wherein said regulator means comprises an air regulator valve connected between said air supply means and said air nozzle, said regulator valve further being connected to sense pressure in said air intake.
 15. The structure of claim 13, wherein said air supply means is connected to respond to the temperature of said engine. 